公开(公告)号：US20140033728A1

公开(公告)日：2014-02-06

申请号：US14048878

申请日：2013-10-08

申请人： ALSTOM Technologies Ltd

发明人： Robert MARMILIC ,  Jaan HELLAT ,  Ewald FREITAG ,  Adnan EROGLU

IPC分类号： F02C3/00

CPC分类号： F02C3/00 ,  F02C7/141 ,  F02C7/228 ,  F05D2220/722 ,  F23R3/346 ,  F23R2900/03341 ,  Y02E20/16 ,  Y02E20/18 ,  Y02T50/671 ,  Y02T50/675

摘要： The invention relates to a gas turbine assembly which substantially includes at least one compressor, at least one first burner, at least one second burner that is connected downstream of the first burner, and at least one turbine that is connected downstream of the second burner. At least the first and second burner form a component of a tubular or quasi-tubular combustion chamber element in the flow direction of the combustion path of the burners. The combustion chamber element being closed or quasi-closed and extending between the compressor and the turbine. The combustion chamber elements are arranged around the rotor of the gas turbine assembly in the shape of a ring.

摘要翻译： 本发明涉及一种燃气轮机组件，其基本上包括至少一个压缩机，至少一个第一燃烧器，连接在第一燃烧器下游的至少一个第二燃烧器和连接在第二燃烧器下游的至少一个涡轮机。 至少第一和第二燃烧器在燃烧器的燃烧路径的流动方向上形成管状或准管状燃烧室元件的部件。 燃烧室元件被关闭或准闭合并且在压缩机和涡轮机之间延伸。 燃烧室元件以环形的形式布置在燃气轮机组件的转子周围。

公开(公告)号：US20130205827A1

公开(公告)日：2013-08-15

申请号：US13642834

申请日：2011-04-19

申请人： Olaf Stallmann

发明人： Olaf Stallmann

IPC分类号： F25J1/00

CPC分类号： F25J1/0027 ,  B01D53/002 ,  B01D2257/504 ,  B01D2258/0283 ,  F25J3/0266 ,  F25J3/067 ,  F25J2200/02 ,  F25J2200/40 ,  F25J2200/70 ,  F25J2200/76 ,  F25J2205/04 ,  F25J2210/70 ,  F25J2215/04 ,  F25J2220/82 ,  F25J2230/04 ,  F25J2230/30 ,  F25J2230/32 ,  F25J2235/80 ,  F25J2240/90 ,  F25J2260/80 ,  F25J2270/02 ,  F25J2270/06 ,  F25J2270/80 ,  F25J2290/62 ,  Y02C10/12 ,  Y02E20/326

摘要： A plant for CO2 separation is described that has a high security level, minimized energy consumption and can deliver liquid CO2 from the flue gas of a fossil fired power plant at different purity levels.

摘要翻译： 描述了一种具有高安全性水平的CO2分离设备，能够最小化能源消耗，并且能够以不同纯度的水平从化石燃煤电厂的烟道气输送液态二氧化碳。

公开(公告)号：US20110038710A1

公开(公告)日：2011-02-17

申请号：US12541266

申请日：2009-08-14

申请人： Dana Kemppainen ,  RuthAnn Rawlings ,  Jonah Klemm-Toole ,  Robert Moore

发明人： Dana Kemppainen ,  RuthAnn Rawlings ,  Jonah Klemm-Toole ,  Robert Moore

IPC分类号： F01D25/08 ,  B05D1/36 ,  F01D5/18

CPC分类号： F01D5/288 ,  C23C4/01 ,  C23C4/02 ,  C23C4/11 ,  C23C4/129 ,  C23C4/134 ,  C23C28/3215 ,  C23C28/3455 ,  F05D2230/80 ,  F05D2230/90

摘要： A configuration for coating a turbine component such as a blade or vane with various forms of thermal barrier coating to provide enhanced temperature capability and increased strain tolerance is disclosed. A gas path surface of the platform, airfoil and airfoil fillet region are first coated with a bond coating. A dense vertically cracked (DVC) thermal barrier coating is then applied to at least the gas path surface of the platform and can be applied to the fillet region. A porous thermal barrier coating is then applied to at least the airfoil. The porous thermal barrier coating can also be applied over the DVC thermal barrier coating if desired.

摘要翻译： 公开了用于涂覆具有各种形式的隔热涂层的涡轮机部件（例如叶片或叶片）以提供增强的温度能力和增加的应变公差的构造。 平台，翼型件和翼型件区域的气体路径表面首先涂覆有粘结涂层。 然后将密集的垂直裂纹（DVC）热障涂层施加到平台的至少气体路径表面，并且可以应用于圆角区域。 然后将多孔热障涂层施加至至少翼型件。 如果需要，多孔隔热涂层也可以涂覆在DVC隔热涂层上。

公开(公告)号：US07780765B2

公开(公告)日：2010-08-24

申请号：US12164400

申请日：2008-06-30

申请人： Srivats Srinivasachar ,  Shin G. Kang ,  Kurt W. Johnson

发明人： Srivats Srinivasachar ,  Shin G. Kang ,  Kurt W. Johnson

IPC分类号： B01D53/02

CPC分类号： B01D53/83 ,  B01D53/10 ,  B01D53/64 ,  B01D2253/102 ,  B01D2257/602 ,  B01J20/20 ,  B01J20/28004 ,  F23J15/003 ,  F23J15/006 ,  F23J2215/60 ,  F23J2217/102 ,  F23J2219/60

摘要： A method for removing mercury from flue gases generated by the combustion of coal comprises: storing a starter batch of activated carbon in an agglomerated state; de-agglomerating the starter batch in a separation device to create a contact batch of activated carbon; transporting the contact batch to a contact location; injecting the contact batch into contact with the flue gas at a contact location having a temperature between 400° F. and 1100° F., whereupon the activated carbon of the contact batch adsorbs mercury from the flue gas; and removing the activated carbon having mercury adsorbed thereon from the flue gas. The transporting step is conducted with substantially no intermediate storage of the contact batch following the de-agglomeration of the starter batch to prevent re-agglomeration of the activated carbon prior to injection.

摘要翻译： 一种从煤燃烧产生的烟道气中去除汞的方法包括：将起始批次的活性炭储存在附聚状态; 将起始物批料在分离装置中去附聚以产生活性炭的接触批料; 将接触批次运送到联系位置; 将接触批料在温度在400°F至1100°F之间的接触位置处与烟道气接触，于是接触批料的活性炭从烟道气中吸附汞; 并从烟道气中除去其上吸附有汞的活性炭。 输送步骤基本上不在起始批次的去附聚之后进行接触批料的中间储存，以防止在注入之前活性炭的再聚集。

公开(公告)号：US20100129196A1

公开(公告)日：2010-05-27

申请号：US12323736

申请日：2008-11-26

申请人： Chris Johnston ,  Gary Bash ,  Tim teRiele ,  David Parker ,  James Page Strohl

发明人： Chris Johnston ,  Gary Bash ,  Tim teRiele ,  David Parker ,  James Page Strohl

IPC分类号： F02C7/12

CPC分类号： F01D5/188 ,  F01D9/041 ,  F02C7/12 ,  F05D2240/81 ,  F05D2260/202 ,  Y10S416/50

摘要： A gas turbine vane to improve vane performance by addressing known failure mechanisms. A cooling circuit to the trailing edge of a vane airfoil is fed from the outer diameter platform, which prevents failure due to an oxidized and eroded airfoil trailing edge. The gas turbine includes an outer diameter platform, a hollow airfoil and an inner diameter platform with a plurality of cooling tubes extending radially through the airfoil. The cooling tubes are open at the outer diameter end and closed with covers at the inner diameter end. The inner diameter platform is also cooled and includes a meterplate for a portion of the cooling passageway and includes an undercut to improve thermal deflections of the inner diameter platform.

摘要翻译： 一种燃气轮机叶片，通过解决已知的故障机制来改善叶片性能。 从外径平台供给到叶片翼型的后缘的冷却回路，这防止由于氧化和侵蚀的翼型后缘造成的故障。 燃气轮机包括外径平台，中空翼型件和具有径向延伸穿过翼型件的多个冷却管的内径平台。 冷却管在外径端开口，在内径端用盖封闭。 内径平台也被冷却，并且包括用于冷却通道的一部分的仪表板，并且包括底切以改善内径平台的热偏转。

公开(公告)号：US20090293444A1

公开(公告)日：2009-12-03

申请号：US12131252

申请日：2008-06-02

申请人： PETER JOHN STUTTAFORD

发明人： PETER JOHN STUTTAFORD

IPC分类号： F02B43/00

CPC分类号： F02C3/28 ,  F02C3/20 ,  F05D2240/36 ,  Y02E20/16

摘要： A system and method for removing at least carbon from a fuel/air mixture prior to injection of the fuel/air mixture into a combustion system is disclosed. The system fully integrates the combined cycle power plant with carbon scrubbing of the fuel/air mixture to increase overall cycle efficiency while capturing carbon from the cycle. A portion of the compressed air source generated by the gas turbine compressor is provided to a premixer where it is mixed with a natural gas to form a fuel/air mixture. The fuel/air mixture passes through a catalytic partial oxidation (CPOX) reactor, which utilizes a precious metal to partially oxidize the hydrocarbons into carbon monoxide. The mixture passes through a shift reactor to complete generation of carbon dioxide and raise hydrogen yield of the fuel/air mixture. Carbon constituents are then removed from the mixture by a separator.

摘要翻译： 公开了一种用于在将燃料/空气混合物注入燃烧系统之前从燃料/空气混合物中去除至少碳的系统和方法。 该系统将联合循环发电厂与燃料/空气混合物的碳清洗完全整合，以提高整体循环效率，同时从循环中捕获碳。 由燃气涡轮压缩机产生的压缩空气源的一部分被提供给预混合器，在该预混合器中与天然气混合以形成燃料/空气混合物。 燃料/空气混合物通过催化部分氧化（CPOX）反应器，其利用贵金属将烃部分氧化成一氧化碳。 混合物通过变换反应器以完成二氧化碳的产生并提高燃料/空气混合物的氢产率。 然后通过分离器从混合物中除去碳成分。

公开(公告)号：US20090290987A1

公开(公告)日：2009-11-26

申请号：US12175822

申请日：2008-07-18

申请人： DAVID PARKER ,  J. PAGE STROHL ,  RICHARD RAMIREZ ,  ROBERT MOORE

发明人： DAVID PARKER ,  J. PAGE STROHL ,  RICHARD RAMIREZ ,  ROBERT MOORE

IPC分类号： F01D5/14

CPC分类号： F01D5/141 ,  F05D2220/3216

摘要： A compressor component having an airfoil with a profile in accordance with Table 1 is disclosed. The compressor component, such as a compressor blade, has an increased thickness over a portion of the airfoil span in order to increase stiffness. Furthermore, the airfoil has been restacked so as to induce a compressive stress in the blade root/attachment area. The increased stiffness and restacked airfoil combine to improve high-cycle fatigue capability of the compressor component.

摘要翻译： 公开了具有根据表1的轮廓的翼型的压缩机部件。 压缩机部件，例如压缩机叶片，在翼型跨度的一部分上具有增加的厚度，以增加刚度。 此外，已经重新安装翼型件以在叶片根部/附接区域中引起压缩应力。 增加的刚度和复位翼型结合起来以改善压缩机部件的高循环疲劳能力。

公开(公告)号：US20090188255A1

公开(公告)日：2009-07-30

申请号：US12247615

申请日：2008-10-08

申请人： Andrew Green ,  Peter Stuttaford ,  Yan Chen ,  Hany Rizkalla

发明人： Andrew Green ,  Peter Stuttaford ,  Yan Chen ,  Hany Rizkalla

IPC分类号： F02C7/12 ,  F23R3/32

CPC分类号： F01D9/023 ,  F23R3/002 ,  F23R3/283 ,  F23R3/286 ,  F23R2900/03041 ,  F23R2900/03044

摘要： A combustor end cap assembly having an improved cooling configuration is disclosed. Embodiments of the present invention are directed towards an apparatus and method for cooling an effusion plate of the combustor end cap assembly. The combustor end cap assembly also incorporates an impingement plate having a plurality of cooling holes with the impingement plate positioned a predetermined distance from the effusion plate. The cooling fluid passes through the impingement plate and is directed towards and onto the effusion plate for cooling of the effusion plate.

摘要翻译： 公开了一种具有改进的冷却结构的燃烧器端盖组件。 本发明的实施例涉及一种用于冷却燃烧器端盖组件的渗出板的装置和方法。 燃烧器端盖组件还包括具有多个冷却孔的冲击板，冲击板定位在距离排出板预定距离处。 冷却流体通过冲击板并且朝向和朝向积液板上并用于冷却渗出板。

公开(公告)号：US09321115B2

公开(公告)日：2016-04-26

申请号：US14173217

申请日：2014-02-05

申请人： Warren Martin Miglietti ,  Emmerson Denver Rene ,  Richard Douglas Konney

发明人： Warren Martin Miglietti ,  Emmerson Denver Rene ,  Richard Douglas Konney

IPC分类号： B23K31/02 ,  B23K1/00 ,  B23P6/00 ,  F01D9/02

CPC分类号： B23K1/0018 ,  B23K2101/001 ,  B23P6/00 ,  B23P6/002 ,  F01D9/023 ,  F05D2230/237 ,  F05D2230/31 ,  F05D2230/80 ,  F23R2900/00019

摘要： The present invention discloses various methods for repairing a side seal region of a transition duct aft frame region. Embodiments of the present invention include application of a braze filler material to worn locations of seal teeth, brazing of a braze preform to the seal teeth or removal of a worn seal tooth and brazing of material compatible with the transition duct to form a replacement tooth of the side seal. The transition duct is brazed in a furnace in an incremental heated process which elevates the transition duct to a temperature where the braze filler material adheres to the side seal region while also providing a stress relief to the transition duct.

摘要翻译： 本发明公开了用于修复过渡管道后框架区域的侧密封区域的各种方法。 本发明的实施例包括将钎焊填充材料应用于密封齿的磨损位置，钎焊预成型件钎焊到密封齿上或去除磨损的密封齿以及与过渡管道相容的材料钎焊以形成替换齿 侧封。 过渡管道以增量加热方式钎焊在炉中，其将过渡管道升高到钎焊填料材料粘附到侧密封区域的温度，同时还向过渡管道提供应力消除。

公开(公告)号：US20130239573A1

公开(公告)日：2013-09-19

申请号：US13847171

申请日：2013-03-19

申请人： ALSTOM TECHNOLOGIES LTD

发明人： Andrea Brighenti ,  Darrel Shayne Lilley ,  Karsten Franitza ,  Anton Nemet

IPC分类号： F01K21/00

CPC分类号： F01K21/00 ,  F01K23/101 ,  F02C6/18 ,  F05D2270/083 ,  F05D2270/0831 ,  F05D2270/303 ,  Y02E20/14 ,  Y02E20/16

摘要： Disclosed is a method for operating a gas turbine (11) comprising a compressor (14), which is equipped with variable inlet guide vanes (13) and receives at its inlet an inlet air flow, which has passed a temperature-affecting air inlet system (12a), a combustor (15, 15′) and a turbine (16, 16′). In a closed loop control scheme, a control variable indicative of the turbine outlet temperature (TAT2) is generated, and the air inlet system (12a) and/or the variable inlet guide vanes (13) are controlled in accordance with said control variable such that the turbine outlet temperature (TAT2) is kept at or above a desired setting value (TAT2min).

摘要翻译： 公开了一种用于操作燃气涡轮机（11）的方法，该燃气涡轮机（11）包括压缩机（14），其配备有可变入口导向叶片（13），并在其入口处接收入口空气流，该入口空气流已经通过温度影响的空气入口系统 （12a），燃烧器（15,15'）和涡轮机（16,16'）。 在闭环控制方案中，产生指示涡轮出口温度（TAT2）的控制变量，并且根据所述控制变量控制进气系统（12a）和/或可变入口导流叶片（13） 涡轮出口温度（TAT2）保持在或高于所需设定值（TAT2min）。